2 fatalities

2011-03-08: De Havilland DHC-6 Twin Otter (N157KM) — Desert Sand Aircraft Leasing — Clayton, United States of America

Clayton, United States of AmericaLanding (descent or approach)

On March 8, 2011, a De Havilland DHC-6 Twin Otter (registration N157KM) operated by Desert Sand Aircraft Leasing was involved in an aviation accident near Clayton, United States of America during landing or approach. 2 people were killed. Investigators recorded the probable cause as: The pilot did not maintain airspeed while maneuvering, which resulted in an aerodynamic stall. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781195579Data APIEditorial standards
Aircraft registered N157KM
Aircraft registered N157KM. Photo: Mehamn / Public domain, via Wikimedia Commons

An airplane that had not been flown for about 5 months crashed after a maintenance test flight following engine replacement. Witnesses observed a stall and impact with trees about 1 mile from the airport. The probable cause was the pilot not maintaining airspeed while maneuvering.

Accident Details

The accident occurred during a maintenance test flight after both engines had been replaced with higher horsepower models. The airplane had not been flown for approximately five months prior to the flight.

Witness Observations

Witnesses reported that the airplane departed and completed two uneventful touch-and-go landings. Subsequently, the aircraft was observed struggling to gain altitude and airspeed while maneuvering in the traffic pattern. One witness, an aircraft mechanic, noted that the airplane was yawing to the left and that he heard noises consistent with propeller pitch changes, which he believed were in the "Beta" range.

The Accident

The airplane stalled and impacted trees in a wooded marsh area, coming to rest about 80 degrees vertically. The accident site was located approximately one mile from the airport.

Wreckage Examination

Examination of the wreckage did not reveal any preimpact malfunctions. However, the lack of flight recorders and the condition of the wreckage precluded the gathering of additional relevant information. Damage observed to both engines and both propellers indicated they were likely operating at symmetrical power settings and blade angles at the time of impact, with any differences in scoring signatures likely resulting from impact damage.

Probable Cause

The official probable cause is that the pilot did not maintain airspeed while maneuvering, which resulted in an aerodynamic stall. The reason for the reported yawing and noise associated with propeller pitch changes prior to the stall could not be determined.